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Awadh B. Pandey, Jupiter US

Awadh B. Pandey, Jupiter, FL US

Patent application numberDescriptionPublished
20090260723High strength L12 aluminum alloys - High strength heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L110-22-2009
20090260724Heat treatable L12 aluminum alloys - High temperature heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L110-22-2009
20090260725Heat treatable L12 aluminum alloys - High temperature heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L110-22-2009
20090263266L12 strengthened amorphous aluminum alloys - An improved amorphous aluminum alloy having high strength, ductility, corrosion resistance and fracture toughness is disclosed. The alloy has an amorphous phase and a coherent L110-22-2009
20090263273High strength L12 aluminum alloys - High temperature heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L110-22-2009
20090263274L12 aluminum alloys with bimodal and trimodal distribution - A two or three phase aluminum alloy having high strength, modulus, ductility and toughness, comprising a fine grain matrix phase nano L110-22-2009
20090263275High strength L12 aluminum alloys - High temperature heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L110-22-2009
20090263276High strength aluminum alloys with L12 precipitates - High strength aluminum magnesium alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L110-22-2009
20090263277Dispersion strengthened L12 aluminum alloys - An improved L110-22-2009
20100139815Conversion Process for heat treatable L12 aluminum aloys - A method for producing high strength aluminum alloy containing L106-10-2010
20100143177Method for forming high strength aluminum alloys containing L12 intermetallic dispersoids - A method and apparatus produces high strength aluminum alloys from a powder containing L106-10-2010
20100226817HIGH STRENGTH L12 ALUMINUM ALLOYS PRODUCED BY CRYOMILLING - A method and apparatus produces high strength aluminum alloys from a cryomilled powder containing L109-09-2010
20100252148HEAT TREATABLE L12 ALUMINUM ALLOYS - High temperature heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L110-07-2010
20100254850CERACON FORGING OF L12 ALUMINUM ALLOYS - A method for producing high strength aluminum alloy consolidated billets containing L110-07-2010
20100282428SPRAY DEPOSITION OF L12 ALUMINUM ALLOYS - A method for producing high strength aluminum alloy product from powder containing L111-11-2010
20100284853DIRECT FORGING AND ROLLING OF L12 ALUMINUM ALLOYS FOR ARMOR APPLICATIONS - A method for producing high strength L111-11-2010
20110017359HIGH STRENGTH L12 ALUMINUM ALLOYS - High strength heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L101-27-2011
20110041963HEAT TREATABLE L12 ALUMINUM ALLOYS - A method of forming high temperature heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L102-24-2011
20110044844HOT COMPACTION AND EXTRUSION OF L12 ALUMINUM ALLOYS - A method and apparatus produces high strength aluminum alloys from a powder containing L102-24-2011
20110052932FABRICATION OF L12 ALUMINUM ALLOY TANKS AND OTHER VESSELS BY ROLL FORMING, SPIN FORMING, AND FRICTION STIR WELDING - A method for producing high strength aluminum alloy tanks and other vessels containing L103-03-2011
20110061494SUPERPLASTIC FORMING HIGH STRENGTH L12 ALUMINUM ALLOYS - A method and apparatus produces high strength aluminum alloys from a powder containing L103-17-2011
20110064599DIRECT EXTRUSION OF SHAPES WITH L12 ALUMINUM ALLOYS - A method for producing a high strength aluminum alloy brackets, cases, tubes, ducts, beams, spars and other parts containing L103-17-2011
20110085932METHOD OF FORMING HIGH STRENGTH ALUMINUM ALLOY PARTS CONTAINING L12 INTERMETALLIC DISPERSOIDS BY RING ROLLING - A method and apparatus produces high strength aluminum alloy parts from a powder containing L104-14-2011
20110088510Hot and cold rolling high strength L12 aluminum alloys - A method and apparatus for producing high strength aluminum alloys from a powder containing Ll04-21-2011
20110091345Method for fabrication of tubes using rolling and extrusion - A method for producing a high strength aluminum alloy tubing containing L104-21-2011
20110091346Forging deformation of L12 aluminum alloys - A method for producing a high strength aluminum alloy parts containing L104-21-2011

Patent applications by Awadh B. Pandey, Jupiter, FL US